ODYSSEY: A Solar System Mission
Christophe, B. and Andersen, P.H. and Anderson, J.D. and Asmar, S. and Bério, Ph. and Bertolami, O. and Bingham, R. and Bondu, F. and Bouyer, P. and Bremer, S. and Courty, J.-M. and Dittus, H. and Foulon, B. and Gil, P. and Johann, U. and Jordan, J.F. and Kent, B. and Lämmerzahl, C. and Lévy, A. and Métris, G. and Olsen, O. and Páramos, J. and Prestage, J.D. and Pogrebenko, S.V. and Rasel, E. and Rathke, A. and Reynaud, S. and Rievers, B. and Samain, E. and Sumner, T.J. and Theil, S. and Touboul, P. and Turyshev, S.G. and Vrancken, P. and Wolf, P. and Yu, N. (2009) ODYSSEY: A Solar System Mission. Experimental Astronomy, 23, pp. 529-547. Springer. DOI: 10.1007/s10686-008-9084-y. ISSN 0922-6435.
Full text not available from this repository.
The Solar System Odyssey mission uses modern-day high-precision experimental techniques to test some the laws questions of fundamental physics which determine dynamics in the solar system. It could lead to a major discoveries by using demonstrated technologies and could be flown within the Cosmic Vision time frame. The mission proposes to perform a set of precision gravitation experiments from the vicinity of Earth to the outer. Its scientific objectives can be summarized as follows: (1) test of gravity force law in the Solar System up to and beyond the orbit Saturn; (2) precise investigation of navigation anomalies at the fly-bys, (3) measurement of Eddington´s parameter at occultation, (4) mapping of gravity field in the outer solar system and study of the Kuiper belt. To aim this, the Odyssey mission is built up on a main spacecraft, designed to fly up to 13 AU, with the following components: (a) a high precision accelerometer, with bias-rejection system, measuring the deviation of the trajectory from the geodesics, that is also giving gravitational forces; (b) Ka-band transponders, as for Cassini, for a precise range and Doppler measurement up to 13 AU, with additional VLBI equipment; (c) optional laser equipment, which would allow one to improve the range and Doppler measurement, resulting in particular in an improved measurement (with respect to Cassini) of the Eddington´s parameter. In this baseline concept, the main spacecraft is designed to operate beyond the Saturn orbit, up to 13 AU. It experiences multiple planetary fly-bys at Earth, Mars, or Venus, and Jupiter. The cruise and fly-by phases allow the mission to schieve its baseline scientific objectives [(1) to (3) in the above list]. In addition to this baseline concept, the Odyssey mission proposes the release of the Enigma radio-beacon at Saturn, allowing one to extend the deep space gravity test up to at least 50 AU, while achieving the scientific objective of a mapping of gravity field in the outer Solar System [(4) in the above list].
|Title:||ODYSSEY: A Solar System Mission|
|Journal or Publication Title:||Experimental Astronomy|
|In ISI Web of Science:||Yes|
|Page Range:||pp. 529-547|
|Keywords:||Gravitation, Relativity, Celestial mechanics, Occultations, Kuiper belt|
|HGF - Research field:||Aeronautics, Space and Transport|
|HGF - Program:||Space|
|HGF - Program Themes:||W - no assignement|
|DLR - Research area:||Space|
|DLR - Program:||W - no assignement|
|DLR - Research theme (Project):||W -- no assignement|
|Institutes and Institutions:||Institute of Space Systems|
|Deposited By:||Prof.Dr. Hansjörg Dittus|
|Deposited On:||24 Feb 2010 13:55|
|Last Modified:||04 Apr 2013 16:20|
Repository Staff Only: item control page